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100   $a20111114j196810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTransonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations /$fby Bobby Lee Berrier and Odis C. Pendergraft, Jr
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Langley Research Center,$dOctober 1968.
215   $a1 online resource (41 pages, 1 unnumbered page) $cillustrations
225 1 $aNASA/TN ;$vD-4843
300   $a"October 1968."
320   $aIncludes bibliographical references (page 11).
606   $aAerospace vehicles$2nasat
606   $aAerodynamic characteristics$2nasat
606   $aMach number$2nasat
606   $aAerodynamics, Transonic$2fast
606   $aMach number$2fast
606   $aSpace vehicles$2fast
615  7$aAerospace vehicles.
615  7$aAerodynamic characteristics.
615  7$aMach number.
615  7$aAerodynamics, Transonic.
615  7$aMach number.
615  7$aSpace vehicles.
700   $aBerrier$b Bobby L.$01389747
702   $aPendergraft$b Odis C.
712 02$aLangley Research Center,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCA
801  2$bGPO
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910715458203321
996   $aTransonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations$93497122
997   $aUNINA